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    Das Bornheimer Depot (auch: Wagenhalle Bornheim, früher: Betriebshof Bornheim) war von bis ein Depot der Frankfurter Straßenbahn. Unmittelbar. Ein Depot (von lateinisch deponere: niederlegen, abstellen), auch Betriebshof, Wagenhalle oder Abstellhalle, ist eine Einrichtung in der Eisenbahnen. The Home Depot, Inc. (börsennotiert an der NYSE, Aktiensymbol: HD, ISIN US, WKN ) ist eine US-amerikanische Baumarktkette mit. BGB auf einen Erwerber. Dies betrifft Bundes- und Landeswertpapiere, ausgenommen Fremdwährungsanleihen diese liegen als Globalurkunde vor. Bei der Wertpapierrechnung befinden sich die Wertpapiere bei denen es sich sowohl um Wertrechte als auch um Urkunden handeln kann nicht im Eigentum des Begünstigten, sondern sie werden von einer ausländischen Stelle als Verwahrer treuhändisch gehalten. Zudem werden sie im Kontoabrufverfahren gemeldet. Oktober um Bei der Wertpapierrechnung befinden sich die Wertpapiere bei denen es sich sowohl um Wertrechte als auch um Urkunden handeln kann nicht im Eigentum des Begünstigten, sondern sie werden von einer ausländischen Stelle als Verwahrer treuhändisch gehalten. Denn diese materiell-rechtliche Vorschrift setzt voraus, dass eine Wertpapierurkunde physisch den Besitzer wechselt. Ansichten Lesen Bearbeiten Quelltext bearbeiten Versionsgeschichte. Entsprechend beruhen Depotgutschriften insbesondere auf Wertpapierkäufen oder —übertragungen, Depotlastschriften auf Wertpapierverkäufen oder —übertragungen. Die Übertragung Verkauf, Schenkung usw. Sie verbrieft ganz oder teilweise eine Wertpapieremission und wird beim Zentralverwahrer verwahrt.

    In the wake of the Joplin tornado in which the walls of a Home Depot collapsed after being hit by an EF5 tornado , The Kansas City Star , citing engineers, criticized Home Depot's practice of using tilt-up construction in hundreds of its big-box stores other nearby big-box stores in Joplin, including a Walmart and Academy Sports , which had concrete block construction, lost their roofs but the walls remained intact.

    In tilt-up construction the concrete is poured onsite, lifted into place, and then attached to the roof. The engineers told the Star that the practice, while normally safe and efficient, is dangerous in major storms because once the roof is lifted as happened in Joplin the walls collapse in a domino effect.

    Seven people were killed in the front of the store when the ,pound walls collapsed on them, while 28 people in the back of the store survived when those walls collapsed outward.

    Only two of the slab walls in the Home Depot survived. In contrast, 3 people died in the Walmart but survived. Engineers noted that when concrete block construction fails, structural elements break in pieces and usually not in huge slabs.

    Home Depot said it fundamentally disagreed with the engineers quoted by the Star and said it would use tilt-up construction when it rebuilds the Joplin store.

    On September 2, , security news reporter Brian Krebs reported that he was seeing evidence of credit card numbers linked to Home Depot purchases being sold online, which he concluded to suggest that The Home Depot's payment systems were breached by hackers.

    According to their press release, this breach affected any customers who made purchases at any Home Depot store from April to September Home Depot offered their affected customers free one-year credit monitoring service from AllClear ID.

    Also in their press release, they made sure to emphasize that there was no evidence to suggest that online customers were affected by the breach.

    On September 18, , Home Depot released a statement saying that the hackers obtained a total of 56 million credit card numbers as a result of the breach.

    Since the breach, Home Depot has rolled out new encryption technology for their cash registers and self-checkout systems to protect customers.

    A class action lawsuit was filed against the company. S Equal Employment Opportunity Commission , for the alleged failure to provide a reasonable accommodation for a cashier with cancer at its Towson, Maryland , store and then for purportedly firing her because of her condition.

    From Wikipedia, the free encyclopedia. The Home Depot, Inc. The Home Depot corporate headquarters outside Atlanta.

    List of data breaches in the United States. March 1, http: Mar 1, http: Retrieved 9 April Archived from the original on February 12, Retrieved July 4, Home Depot Corporate website: Archived from the original on June 26, Retrieved June 11, Archived from the original on September 4, Retrieved September 3, Archived from the original on January 23, Retrieved April 11, Retrieved 21 April Retrieved 22 April The New York Times.

    Retrieved August 5, Retrieved January 19, Retrieved April 29, Retrieved May 19, Retrieved September 21, Retrieved July 22, Retrieved 26 April The Orange County Register.

    Retrieved 22 August Retrieved 21 January Retrieved 13 October Archived from the original on November 1, Retrieved June 9, Georgia College and State University.

    Pleasant American Legion building gets improved by volunteers". Retrieved October 1, Retrieved August 22, Retrieved May 25, Retrieved September 12, Retrieved June 23, Archived from the original on January 21, Retrieved October 24, Archived from the original on February 6, The Wall Street Journal.

    Retrieved 19 February Archived from the original on October 29, Retrieved January 1, Archived from the original on November 17, Archived from the original on October 15, Securities and Exchange Commission.

    Additionally, the original slate roof was replaced by copper plates due to leaking problems. Most of the building is not used for its original purpose, but Union Pacific uses some of the space for offices and training areas.

    In January , three floors opened as a restaurant and music venue, fittingly called The Depot. From Wikipedia, the free encyclopedia. Redirected from The Depot.

    For other uses, see The Depot disambiguation. National Register of Historic Places. Federal Reserve Bank of Minneapolis. Retrieved January 2, Retrieved 9 Jan Retrieved 21 August Further, long life components including insulation, power and cryocoolers could be placed on the depot and not expended, further reducing the mass per mission and hence costs.

    Both theoretical studies and funded development projects that are currently underway provide answers to the "Are propellant depots feasible?

    In a NASA study, an additional flight of a " Ares V heavy " launch vehicle was required to stage a US government Mars reference mission due to 70 tons of boiloff, assuming 0.

    Approaches to the design of low Earth orbit LEO propellant depots were also discussed in the Augustine report to NASA , which "examined the [then] current concepts for in-space refueling.

    Both approaches were considered feasible with spaceflight technology, but anticipated that significant further engineering development and in-space demonstration would be required before missions could depend on the technology.

    Both approaches were seen to offer the potential of long-term life-cycle savings. Beyond theoretical studies, since at least , SpaceX has undertaken funded development of an interplanetary set of technologies called the Interplanetary Transport System ITS.

    While the system consists of a combination of several elements that are considered by SpaceX to be key to making long-duration beyond Earth orbit BEO spaceflights possible by reducing the cost per ton delivered to Mars by multiple orders of magnitude over what NASA approaches have achieved, [14] [15] [16] refilling of propellants in orbit is one of the four key elements.

    In a novel mission architecture, the SpaceX design intends to enable the long-journey spacecraft to expend most all of its propellant load during the launch to low Earth orbit while it serves as the second stage of the launch vehicle , and then—after refilling on orbit by an ITS tanker —provide the significant amount of energy necessary to put the spacecraft onto an interplanetary trajectory.

    A second propellant tanker concept is underway. Because a large portion of a rocket is propellant at time of launch, proponents point out several advantages of using a propellant depot architecture.

    Spacecraft could be launched unfueled and thus require less structural mass, [21] or the depot tanker itself could serve as the second-stage on launch when it is reusable.

    Propellant depots were proposed as part of the Space Transportation System along with nuclear "tugs" to take payloads from LEO to other destinations in the mids.

    The post-spacecraft mission extension ran 2. ULA is also currently planning additional in-space laboratory experiments to further develop cryogenic fluid management technologies using the Centaur upper stage after primary payload separation.

    The Future In-Space Operations FISO Working Group, a consortium of participants from NASA, industry and academia, discussed propellant depot concepts and plans on several occasions in , [32] with presentations of optimal depot locations for human space exploration beyond low Earth orbit, [33] a proposed simpler single vehicle first-generation propellant depot [30] and six important propellant-depot-related technologies for reusable cislunar transportation.

    Simple Depot would utilize the "used" nearly-emptied Centaur upper stage LH2 tank for long-term storage of LO2 while LH2 will be stored in the Simple Depot LH2 module, which is launched with only ambient-temperature gaseous Helium in it.

    The SD LH2 tank was to be 3 metres 9. The concept proposes that waste gaseous hydrogen —an inevitable byproduct of long-term liquid hydrogen storage in the radiative heat environment of space —would be usable as a monopropellant in a solar-thermal propulsion system.

    The waste hydrogen would be productively utilized for both orbital stationkeeping and attitude control , as well as providing limited propellant and thrust to use for orbital maneuvers to better rendezvous with other spacecraft that would be inbound to receive fuel from the depot.

    ACES hardware is designed from the start to as an in-space propellant depot that could be used as way-stations for other rockets to stop and refuel on the way to beyond-LEO or interplanetary missions, and to provide the high-energy technical capacity for the cleanup of space debris.

    In August , NASA made a significant contractual commitment to the development of propellant depot technology [1] by funding four aerospace companies to "define demonstration missions that would validate the concept of storing cryogenic propellants in space to reduce the need for large launch vehicles for deep-space exploration.

    There are a number of design issues with propellant depots, as well as several tasks that have not, to date, been tested in space for on-orbit servicing missions.

    Transfer of liquid propellants in microgravity is complicated by the uncertain distribution of liquid and gasses within a tank.

    Propellant settling at an in-space depot is thus more challenging than in even a slight gravity field. ULA plans to use the DMSP mission to flight-test centrifugal propellant settling as a cryogenic fuel management technique that might be used in future propellant depots.

    In the absence of gravity, propellant transfer is somewhat more difficult, since liquids can float away from the inlet. As part of the Orbital Express mission in , hydrazine propellant was successfully transferred between two single-purpose designed technology demonstration spacecraft.

    Since no crew were present on either spacecraft, this was reported as the first autonomous spacecraft-to-spacecraft fluid transfer. After propellant has been transferred to a customer the depot's tanks will need refilling.

    Organizing the construction and launch of the tanker rockets bearing the new fuel is the responsibility of the propellant depot's operator.

    By using several tanker rockets the tankers can be smaller than the depot and larger than the spacecraft they are intended to resupply.

    Short range chemical propulsion tugs belonging to the depot may be used to simplify docking tanker rockets and large vehicles like Mars Transfer Vehicles.

    Transfers of propellant between the LEO depot, reachable by rockets from Earth, and the deep space ones such as the Lagrange Points and Phobos depots can be performed using Solar electric propulsion SEP tugs.

    Two missions are currently under development or proposed to support propellant depot refilling. In addition to refueling and servicing geostationary communications satellites with the fuel that is initially launched with the MDA Space Infrastructure Servicing vehicle, the SIS vehicle is being designed to have the ability to orbitally maneuver to rendezvous with a replacement fuel canister after transferring the kg of fuel in the launch load, enabling further refueling of additional satellites after the initial multi-satellite servicing mission is complete.

    Demetriades [44] proposed a method for refilling by collecting atmospheric gases. The remaining nitrogen is used as propellant for a nuclear-powered magnetohydrodynamic engine, which maintains the orbit, compensating for atmospheric drag.

    However, Jones' proposal does require a network of orbital power-beaming satellites , to avoid placing nuclear reactors in orbit.

    Asteroids can also be processed to provide liquid oxygen. Propellant depots in LEO are of little use for transfer between two low earth orbits when the depot is in a different orbital plane than the target orbit.

    The delta-v to make the necessary plane change is typically extremely high. On the other hand, depots are typically proposed for exploration missions, where the change over time of the depot's orbit can be chosen to align with the departure vector.

    This allows one well-aligned departure time minimizing fuel use that requires a very precisely-timed departure.

    Less efficient departure times from the same depot to the same destination exist before and after the well-aligned opportunity, but more research is required to show whether the efficiency falls off quickly or slowly.

    The restrictions on departure windows arise because low earth orbits are susceptible to significant perturbations; even over short periods they are subject to nodal regression and, less importantly, precession of perigee.

    Equatorial depots are more stable but also more difficult to reach. However, it is possible to do a three-burn orbital transfer which includes a plane change, and which wastes very little propellant to reach almost any final trajectory.

    Boil-off of cryogenic propellants in space may be mitigated by both technological solutions as well as system-level planning and design.

    From a technical perspective: Boil off rate is governed by heat leakage and by the quantity of propellant in the tanks. With partially filled tanks, the percentage loss is higher.

    Heat leakage depends on surface area, while the original mass of propellant in the tanks depends on volume. So by the cube-square law , the smaller the tank, the faster the liquids will boil off.

    Some propellant tank designs have achieved a liquid hydrogen boil off rate as low as approximately 0. It is possible to achieve zero boil-off ZBO with cryogenic propellant storage using an active thermal control system.

    Liquid hydrogen was the test fluid. The test tank was installed into a vacuum chamber, simulating space vacuum. A commercial cryocooler was interfaced with an existing MHTB spray bar mixer and insulation system in a manner that enabled a balance between incoming and extracted thermal energy.

    Another NASA study in June for conceptual Mars mission showed mass savings over traditional, passive- only cryogenic storage when mission durations are 5 days in LEO for oxygen, 8.

    Longer missions equate to greater mass savings. Cryogenic xenon saves mass over passive storage almost immediately. When power to run the ZBO is already available, the break-even mission durations are even shorter, e.

    Archived handball recken the original on Wm skispringen 2019 7, The New Beste Spielothek in Schwaighausen finden Times. The change occurred on November 1, An Office Depot store in Thornhill, Ontario. September Learn how and when to remove this template message. The financial difficulties of The Home Depot also caused the stock price to fall. Bruce, J Graeme Transfers of propellant between handball recken LEO depot, reachable by cs go big pot from Earth, and the deep craps casino regeln ones such as the Lagrange Points and Phobos depots can be performed using Solar electric propulsion SEP tugs. Although a longtime deputy to Nardelli at GE and Home Depot, Blake was said to lack Nardelli's hard edge and instead preferred to make decisions by consensus. Sixty Years of the Northern. S Equal Employment Opportunity Beste Spielothek in Wildenthal findenfor the alleged failure gutschein casino zollverein provide a reasonable accommodation for a cashier with cancer at its Towson, Marylandstore and Battle of the Atlantic Slots - Find Out Where to Play Online for purportedly firing her because of her condition. Views Read Edit View history. The Home Depot Foundation is the philanthropic arm of the company created in This page was last edited on 7 Octoberat Archived from the original on February 12, Seit diesem Zeitpunkt gibt es also für die Aktiengesellschaften ultra hot deluxe Möglichkeit, wirksam zu verhindern, dass noch Einzelurkunden in Umlauf kommen. Depotguthaben weisen den Bestand an genau bezeichneten Wertpapieren aus, den der Kontoinhaber beim kontoführenden Kreditinstitut unterhält. Navigation Hauptseite Themenportale Zufälliger Artikel. Position aufgelöst, Kriterien nicht mehr erfüllt. Bei der Sammelverwahrung ist nach Haussammeldepot und Girosammeldepot zu unterscheiden.

    Transfer of liquid propellants in microgravity is complicated by the uncertain distribution of liquid and gasses within a tank.

    Propellant settling at an in-space depot is thus more challenging than in even a slight gravity field. ULA plans to use the DMSP mission to flight-test centrifugal propellant settling as a cryogenic fuel management technique that might be used in future propellant depots.

    In the absence of gravity, propellant transfer is somewhat more difficult, since liquids can float away from the inlet. As part of the Orbital Express mission in , hydrazine propellant was successfully transferred between two single-purpose designed technology demonstration spacecraft.

    Since no crew were present on either spacecraft, this was reported as the first autonomous spacecraft-to-spacecraft fluid transfer.

    After propellant has been transferred to a customer the depot's tanks will need refilling. Organizing the construction and launch of the tanker rockets bearing the new fuel is the responsibility of the propellant depot's operator.

    By using several tanker rockets the tankers can be smaller than the depot and larger than the spacecraft they are intended to resupply. Short range chemical propulsion tugs belonging to the depot may be used to simplify docking tanker rockets and large vehicles like Mars Transfer Vehicles.

    Transfers of propellant between the LEO depot, reachable by rockets from Earth, and the deep space ones such as the Lagrange Points and Phobos depots can be performed using Solar electric propulsion SEP tugs.

    Two missions are currently under development or proposed to support propellant depot refilling. In addition to refueling and servicing geostationary communications satellites with the fuel that is initially launched with the MDA Space Infrastructure Servicing vehicle, the SIS vehicle is being designed to have the ability to orbitally maneuver to rendezvous with a replacement fuel canister after transferring the kg of fuel in the launch load, enabling further refueling of additional satellites after the initial multi-satellite servicing mission is complete.

    Demetriades [44] proposed a method for refilling by collecting atmospheric gases. The remaining nitrogen is used as propellant for a nuclear-powered magnetohydrodynamic engine, which maintains the orbit, compensating for atmospheric drag.

    However, Jones' proposal does require a network of orbital power-beaming satellites , to avoid placing nuclear reactors in orbit. Asteroids can also be processed to provide liquid oxygen.

    Propellant depots in LEO are of little use for transfer between two low earth orbits when the depot is in a different orbital plane than the target orbit.

    The delta-v to make the necessary plane change is typically extremely high. On the other hand, depots are typically proposed for exploration missions, where the change over time of the depot's orbit can be chosen to align with the departure vector.

    This allows one well-aligned departure time minimizing fuel use that requires a very precisely-timed departure. Less efficient departure times from the same depot to the same destination exist before and after the well-aligned opportunity, but more research is required to show whether the efficiency falls off quickly or slowly.

    The restrictions on departure windows arise because low earth orbits are susceptible to significant perturbations; even over short periods they are subject to nodal regression and, less importantly, precession of perigee.

    Equatorial depots are more stable but also more difficult to reach. However, it is possible to do a three-burn orbital transfer which includes a plane change, and which wastes very little propellant to reach almost any final trajectory.

    Boil-off of cryogenic propellants in space may be mitigated by both technological solutions as well as system-level planning and design.

    From a technical perspective: Boil off rate is governed by heat leakage and by the quantity of propellant in the tanks. With partially filled tanks, the percentage loss is higher.

    Heat leakage depends on surface area, while the original mass of propellant in the tanks depends on volume. So by the cube-square law , the smaller the tank, the faster the liquids will boil off.

    Some propellant tank designs have achieved a liquid hydrogen boil off rate as low as approximately 0. It is possible to achieve zero boil-off ZBO with cryogenic propellant storage using an active thermal control system.

    Liquid hydrogen was the test fluid. The test tank was installed into a vacuum chamber, simulating space vacuum. A commercial cryocooler was interfaced with an existing MHTB spray bar mixer and insulation system in a manner that enabled a balance between incoming and extracted thermal energy.

    Another NASA study in June for conceptual Mars mission showed mass savings over traditional, passive- only cryogenic storage when mission durations are 5 days in LEO for oxygen, 8.

    Longer missions equate to greater mass savings. Cryogenic xenon saves mass over passive storage almost immediately. When power to run the ZBO is already available, the break-even mission durations are even shorter, e.

    In addition to technical solutions to the challenge of excessive boil-off of cryogenic rocket propellants, system-level solutions have been proposed.

    Such proposals have been suggested as supplementing good technological techniques to reduce boil-off, but would not replace the need for efficient technological storage solutions.

    United Launch Alliance ULA has proposed a cryogenic depot which would use a conical sun shield to protect the cold propellants from solar and Earth radiation.

    The open end of the cone allows residual heat to radiate to the cold of deep space, while the closed cone layers attenuates the radiative heat from the Sun and Earth.

    Other issues are hydrogen embrittlement , a process by which some metals including iron and titanium become brittle and fracture following exposure to hydrogen.

    The resulting leaks makes storing cryogenic propellants in zero gravity conditions difficult. In the early s, several in-space refueling projects got under-way.

    Two private initiatives and a government-sponsored test mission were in some level of development or testing as of [update].

    The NASA Robotic Refueling Mission was launched in and successfully completed a series of robotically-actuated propellant transfer experiments on the exposed facility platform of the International Space Station in January The set of experiments included a number of propellant valves , nozzles and seals similar to those used on many satellites and a series of four prototype tools that could be attached to the distal end of a Space Station robotic arm.

    Each tool was a prototype of "devices that could be used by future satellite servicing missions to refuel spacecraft in orbit.

    RRM is the first in-space refueling demonstration using a platform and fuel valve representative of most existing satellites, which were never designed for refueling.

    Other satellite servicing demos, such as the U. Canada -based MDA Corporation announced in early that they were designing a single spacecraft that would refuel other spacecraft in orbit as a satellite-servicing demonstration.

    Competitive design alternatives to in-space RCS fuel transfer exist. It is possible to bring additional propellant to a space asset, and utilize the propellant for attitude control or orbital velocity change, without ever transferring the propellant to the target space asset.

    The ViviSat Mission Extension Vehicle , also under development since the early s, illustrates one alternative approach that would connect to the target satellite similarly to MDA SIS, via the kick motor, but will not transfer fuel.

    Rather, the Mission Extension Vehicle will use "its own thrusters to supply attitude control for the target. In , Lockheed Martin proposed the Jupiter space tug.

    If built, Jupiter would operate in low Earth orbit shuttling cargo carriers to and from the International Space Station , remaining on orbit indefinitely, and refueling itself from subsequent transport ships carrying later cargo carrier modules.

    From Wikipedia, the free encyclopedia. IAC - 12, D3, 2, 4 , x Retrieved October 14, Retrieved January 24, American Institute of Aeronautics and Astronautics.

    Lauderdale, FL, July 11—14, Ad Astra Rocket Company. Archived from the original on May 22, Archived from the original PDF on July 4, Retrieved February 21, Human Spaceflight Plans Committee , p.

    Making Humans a Multiplanetary Species video. Event occurs at 9: Retrieved October 18, So it is a bit tricky. Because we have to figure out how to improve the cost of the trips to Mars by five million percent Archived from the original PDF on September 28, Retrieved October 9, Retrieved October 31, It leverages design features of both the Centaur and Delta Cryogenic Second Stage DCSS upper stages and intends to supplement and perhaps replace these stages in the future.

    The baseline mT propellant load is contained in a 5m diameter, common bulkhead stage that is about the same length as ULA's existing upper stages.

    ACES will become the foundation for a modular system of stages to meet the launch requirements of a wide variety of users. A common variant is a stretched version containing 73 t of propellant.

    Retrieved November 10, Archived July 17, , at the Wayback Machine. Retrieved September 11, Retrieved August 11, Archived from the original PDF on July 17, Retrieved January 25, A practical depot must evolve hydrogen at a minimum rate that matches the station keeping demands.

    China Achieves Orbital Refueling". Retrieved July 10, Archived from the original on May 5, Archived from the original on March 21, Redirected from The Depot.

    For other uses, see The Depot disambiguation. National Register of Historic Places. Federal Reserve Bank of Minneapolis. Retrieved January 2, Retrieved 9 Jan Retrieved 21 August District of Columbia Morocco.

    Retrieved from " https: Views Read Edit View history. In other projects Wikimedia Commons. This page was last edited on 21 August , at By using this site, you agree to the Terms of Use and Privacy Policy.

    Former Union Pacific Railroad and Amtrak station. Union Pacific Depot c. California Zephyr Before reroute.

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